06 HYDRAULICS, FLIGHT CONTROLS, LANDING GEAR, BRAKES
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1 Course overview N E X T G E N E R A T I O N Airplane General Air Systems Warning Systems, Communications, Ice & Rain Protection Electrical Engines, APU, Fuel System Hydraulics, Flight Controls, Landing Gear, Brakes Flight Instruments & Displays Automatic Flight Flight Management, Navigation Normal Operations Topics Overview Roll control Ailerons Flight spoilers Pitch control Elevators Stabilizer Stalls Yaw control Rudder Yaw damper Speed brakes Flaps & slats Overview Hydraulic power distribution A & B systems System leaks Power transfer unit Landing gear transfer unit Standby system Landing gear & brakes Landing gear operation Brake system Air/Ground system Overview The airplane has three hydraulic systems: A, B and standby. The standby system is used if system A and/or B pressure is lost. The hydraulic systems power the following systems: flight controls leading edge flaps and slats trailing edge flaps landing gear wheel brakes nose wheel steering thrust reversers autopilots Either A or B hydraulic system can power all flight controls with no decrease in airplane controllability. Each hydraulic system has a fluid reservoir located in the main wheel well area. System A and B reservoirs are pressurized by bleed air. The standby system reservoir is connected to the system B reservoir for pressurization and servicing. Pressurization of all reservoirs ensures positive fluid flow to all hydraulic pumps. Controls & indicators: Hydraulic panel Controls & indicators: Indications (DU) Caution (amber) operating limit (red) System pressure indication ELEC hyd pump overheat lights Hyd pump LOW PRESS lights ELEC hyd pump ENG hyd pump Caution (amber) operating limit (red) Sys quantity indication Refill indication 1
2 Main wheel well Control & indicators: Flight control panel SYSTEM A & B reservoirs Pressure gauge Flight Control Flight Control LOW PRESSURE lights Standby hyd LOW QUANTITY light Standby hyd LOW PRESSURE light Standby rudder ON light Alternate Flaps master switch Hydraulic Power Distribution A & B systems Components powered by hydraulic systems A and B: System A ailerons rudder elevator and elevator feel flight spoilers (two on each wing) ground spoilers alternate brakes No. 1 thrust reverser autopilot A normal nose wheel steering landing gear power transfer unit (PTU) System B ailerons rudder elevator and elevator feel flight spoilers (two on each wing) leading edge flaps and slats normal brakes No. 2 thrust reverser autopilot B alternate nose wheel steering landing gear transfer unit. autoslats yaw damper trailing edge flaps. Standby system Overview Flight control surfaces location 2
3 Control & indicators: Flight control panel Control & indicators: LE devices LE devices TRANSIT light Flight Control Flight Control LOW PRESSURE lights Standby hydraulic system lights Alternate Flaps master switch Alternate Flaps position switch LE devices EXTENDED light LE devices FULL EXT light Flight Spoiler Yaw Damper light Feel Differential Pressure light Speed Trim Failure light Mach Trim Failure light Automatic Slat Failure light LE panel test switch Yaw Damper switch Control & indicators: Stabilizer Roll Control Stab Trim Wheel (Control Stand) Stab Trim Indicator Stab Trim Green band range Stab Trim Switches (Control Wheel) Stab Trim Main Elec Cutout Switch (Control Stand) Stab Trim Autopilot Cutout Switch (Control Stand) Stab Trim Override Switch Stab Out of Trim light Pitch Control Yaw Control 3
4 Speed Brakes LE devices & TE flaps Nose landing gear Main landing gear Controls & indicators: Landing gear panel Autobrake & antiskid controls Indications 4
5 Indications Main landing gear (photo) Pushback procedures Köszönöm a figyelmet! Copyright 2005 Malev Virtual Training Division. All rights reserved. Elérhetõségek: Internet: training@virtualairlines.hu Elõadó: Hegedüs Zoltán 5
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